• Structural Engineering and Mechanics
• /
• 제56권5호
• /
• pp.835-854
• /
• 2015

In this paper, the modified form of shear deformation plate theories is proposed. First, the displacement field geometry of classical and the first order shear deformation theories are compared with each other. Using this comparison shows that there is a kinematic relation among independent variables of the first order shear deformation theory. So, the modified forms of rotation functions in shear deformation theories are proposed. Governing equations for rectangular and circular thick laminated plates, having been analyzed numerically so far, are solved by method of separation of variables. Natural frequencies and mode shapes of the plate are determined. The results of the present method are compared with those of previously published papers with good agreement obtained. Efficiency, simplicity and excellent results of this method are extensible to a wide range of similar problems. Accurate solution for governing equations of thick composite plates has been made possible for the first time.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2006년도 추계 학술대회논문집
• /
• pp.11-12
• /
• 2006

We conducted a direct numerical simulation (DNS) to establish database for the purpose of improvement of practical method which is applicable to cavitating turbulent flows. Cavitations caused by spanwise and streamwise vortices, which are typical features in high shear layer, is represented by a simple model and interaction between vortices and cavities is reproduced. The qualitative agreement between computation and experiment are reasonable. Cavities due to streamwise vortices in a shear layer seem to attenuate turbulent eddies.

• 한국수소및신에너지학회논문집
• /
• 제31권6호
• /
• pp.578-586
• /
• 2020

There is growing interest worldwide in a hydrogen economy that uses hydrogen as an energy medium instead of hydrocarbon-based fossil fuels as a way to combat climate change. Since hydrogen has a very low energy density per unit volume at room temperature, hydrogen must be compressed and stored in order to use as an energy carrier. There are mechanical and non-mechanical methods for compressing hydrogen. The mechanical method has disadvantages such as high energy consumption, durability problems of moving parts, hydrogen contamination by lubricants, and noise. Among the non-mechanical compression methods, electrochemical compression consumes less energy and can compress hydrogen with high purity. In this paper, research trends are reviewed, focusing on research papers on electrochemical hydrogen compression technology, and future research directions are suggested.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
• /
• pp.192-197
• /
• 2004

Recently, fluidic thrust vectoring methods have been preferably employed to control the movement of propulsive systems due to relatively simpler design and lower cost than mechanical thrust vectoring methods. For An application of the thrust vectoring to flight bodies, it is necessary to understand very complicated exhaust flows which are often subject to shock waves and boundary layer separation. But researches for the thrust vector control using counterflow have been few. In the present study, experiments have been performed to investigate the characteristics of supersonic jets controlled by a thrust vectoring method using counterflow. The primary jet is expanded through a two-dimensional primary nozzle shrouded by collars, and is deflected by the suction of the air near nozzle into an upper slot placed between the primary nozzle and the upper collar. A shadowgraph method is used to visualize the supersonic jet flowfields. Primary nozzle pressure ratios and suction nozzle pressure ratios are varied from 3.0 to 5.0, and from 0.2 to 1.0 respectively. The present experimental results showed that, for a given primary nozzle pressure ratio, a decrease in the suction nozzle pressure ratio produced an increased thrust vector angle. As the suction nozzle pressure ratios were increased and decreased, the hysteresis of the thrust vectoring was observed through the wall pressure distributions

• 대한기계학회논문집A
• /
• 제36권11호
• /
• pp.1473-1478
• /
• 2012

본 논문은 원거리에 떨어진 작전지역으로 정찰로봇을 발사하여 투하하기 위해서 필요한 파단형 보호체에 대한 개발내용을 제시한다. 실제 전장에서의 활용성을 높이기 위해 기존 외피 전개를 위한 기구사용을 배제하고 체결부의 파단에 의해서 보호체의 외피가 개방되는 방식을 채택하여 소형, 경량을 이루었다. 보호체와 정찰로봇의 유한요소 모델링을 통해서 주어진 하중조건에 맞추어 체결부의 파단이 이루어지는지 전산모의실험을 수행하였으며, 낙하시험기를 이용한 충격실험을 통해서 충돌에 대한 보호체의 충격흡수성능을 분석하였다. 실제 외부환경에서의 100m 발사시험을 통해서 제안된 보호체가 정찰로봇을 탑재하여 정해진 지점으로 비행 도착한 후 안전하게 정찰로봇을 이탈시킴을 확인하였다.

• 대한기계학회논문집B
• /
• 제22권3호
• /
• pp.373-385
• /
• 1998

The local Nusselt numbers have been measured for a round turbulent jet impinging on the convex surface with and without rib. Liquid crystal/transient method was used to determine the Nusselt number distributions along the surface. The temperature on the surface was measured to within .+-.0.25 deg. C accuracy using liquid crystal and a digital color image processing system. The experiments were made for the jet Reynolds number (Re) 23,000, the dimensionless nozzle-to-surface distance (L/d) from 6 to 10, the dimensionless surface curvature (d/D) 0.056, and the various rib types (height(d$_{1}$) from 1 to 2 mm, pitch (p) from 6 to 32 mm). It was found that the average Nusselt numbers on the convex surface with rib are higher than those without rib, mainly due to an increase in the turbulent intensity caused by flow separation, recirculation and reattachment on the wall surface. In addition, we compared the results by the steady-state method using the gold-film Intrex with those by the transient method.

• 대한기계학회논문집B
• /
• 제37권3호
• /
• pp.259-266
• /
• 2013

광학 현미경을 통해 일정한 시간 간격으로 얻은 세포 이미지로부터 세포 변화를 자동적으로 추적 및 분석하는 것이 세포 트래킹이라고 한다. 세포 변화 과정에서 이웃에 있는 세포들이 겹쳐져 있는 상태를 클러스터라고 하며 세포트래킹에서 클러스터를 다시 세포로 분리하는 작업은 매우 중요하다. 본 논문에서는 타원 근사법을 기반으로 클러스터를 분리하기 위한 알고리즘을 제안한다. 클러스터의 외곽선을 추출한 후 외곽선의 오목정점을 이용하여 클러스터를 라인 세그먼트들로 분리한 다음 휴리스틱을 이용하여 라인 세그먼트들을 결합해 가며 근사 타원을 생성한다. 실험 결과 두 개의 세포가 겹쳐진 클러스터의 경우 평균적으로 91%, 세 개의 세포가 겹쳐진 경우 평균적으로 84% 그리고 겹쳐진 세포의 개수가 네 개 이상인 경우 약 73%의 정확도로 클러스터를 분리해 주었다.

• 대한기계학회논문집
• /
• 제17권12호
• /
• pp.3135-3147
• /
• 1993

A numerical method is presented which can solve the steady flow and heat transfer from a rotating and heated circular cylinder in a uniform flow for a range of Reynolds number form 5 to 100. The steady response of the flow and heat transfer is simulated for various spin parameter. The effects on the flow field and heat transfer characteristics known as lift, drag and heat transfer coefficient are analyzed and the streamlines, velocity vectors, vorticity, temperature distributions around it were scrutinized numerically. As spin parameter increases the region of separation vortex becomes smaller than upper one and the lower region will vanish. The lift force, a large part is due to the pressure force, increases as the Reynolds number and it increases linearly as spin parameter increases. The pressure coefficient changes rapidly with spin parameter on the lower surface of the cylinder and the vorticity is sensitive to the spin parameter near separation region. As spin parameter increases the maximum heat coefficient and the thin thermal layer on front region are moved to direction of rotation. However, with balance between the local increase and decrease, the overal heat transfer coefficient is almost unaffected by rotation.

• 대한기계학회논문집
• /
• 제12권3호
• /
• pp.590-598
• /
• 1988

본 연구에서는 난류유동이론을 적용하여 2차원 스크린의 후류에 관한 유동특 성을 연구하였다. 이를 위해 적합한 난류모델 및 스크린의 존재를 고려한 수치해석 방법을 연구하였다. 스크린의 저항이 커서 스크린 하류유동이 역류가 되는 경우도 포함하였다.

• 대한기계학회논문집A
• /
• 제28권8호
• /
• pp.1135-1139
• /
• 2004

This paper presents a microextractor for the separation of DNA molecules by their sizes. The DNA microextractor immobilizes the DNA molecules of specific size in the micropillar array by adjusting the period of the crossed electric field, thus providing a starting-point independent target DNA extraction method without separation process monitoring. The DNA microextractor has been fabricated by a three-mask micromachining process. The velocity of three different DNA molecules has been measured at the electric field of E=5V/0.8cm in the fabricated DNA microextractor, resulting in the reorientation times of $4.80{\pm}0.44sec,\;7.12{\pm}0.75sec$, and $9.88{\pm}0.30sec$ for ${\lambda}$ DNA, micrococcus DNA, and T4 DNA, respectively. T4 DNA is trapped in the micropillar array when the crossed electric field of 5V/0.8cm is applied alternately at a 10 second time interval. The present DNA microextractor filters the DNA in a specific size range by adjusting the magnitude and/or the period of the crossed electric field applied in the micropillar array.